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Flight test techniques for the X-29A aircraftThe X-29A advanced technology demonstrator is a single-seat, single-engine aircraft with a forward-swept wing. The aircraft incorporates many advanced technologies being considered for this country's next generation of aircraft. This unusual aircraft configuration, which had never been flown before, required a precise approach to flight envelope expansion. This paper describes the real-time analysis methods and flight test techniques used during the envelope expansion of the x-29A aircraft, including new and innovative approaches.
Document ID
19870012475
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hicks, John W.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Cooper, James M., Jr.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Sefic, Walter J.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1987
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
H-1401
NASA-TM-88289
NAS 1.15:88289
AIAA PAPER 87-0082
Report Number: H-1401
Report Number: NASA-TM-88289
Report Number: NAS 1.15:88289
Report Number: AIAA PAPER 87-0082
Accession Number
87N21908
Funding Number(s)
PROJECT: RTOP 533-02-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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